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公开(公告)号：US08752398B2
公开(公告)日：2014-06-17
申请号：US12790284
申请日：2010-05-28
CPC分类号： F25B41/00 , B64D13/08 , B64D2013/0674 , F25B2400/0401 , F25B2400/0411 , F25B2600/0251 , F25B2700/2106 , F25B2700/2116 , Y02T50/56
摘要： The invention relates to a refrigerating device (10), in particular for an aircraft, having a refrigerant circuit, in which a refrigerant container (12), an expansion valve (14), an evaporator (16), a compressor (20) and a condenser (22) are disposed. To save energy during operation and to increase the reliability and availability of the refrigerating device (10), in the refrigerant circuit there is a compressor bypass line (26), in which a bypass valve (18) is disposed, and a refrigerant pump (30) that is disposed downstream of the condenser (22) and upstream of the evaporator (16). It is possible to dispense with the refrigerant pump (30) if the condenser (22) is disposed at a higher level than the evaporator (16) in the refrigerant circuit.
摘要翻译： 本发明涉及具有制冷剂回路的制冷装置（10），特别是用于航空器的制冷装置（10），其中制冷剂容器（12），膨胀阀（14），蒸发器（16），压缩机（20）和 设置冷凝器（22）。 为了节省运转时的能量，提高制冷装置（10）的可靠性和可利用性，在制冷剂回路中设置有配置有旁通阀（18）的压缩机旁通管路（26）和制冷剂泵 30），其设置在冷凝器（22）的下游和蒸发器（16）的上游。 如果冷凝器（22）设置在比制冷剂回路中的蒸发器（16）更高的高度，则可以省略制冷剂泵（30）。
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2.发明申请AIRCRAFT COOLING SYSTEM EVAPORATOR ARRANGEMENT FOR TWO MUTUALLY INDEPENDENT COOLANT CIRCUITS 有权两台独立冷凝器电路的飞机冷却系统蒸发器布置公开(公告)号：US20110107782A1
公开(公告)日：2011-05-12
申请号：US12675278
申请日：2008-09-01
CPC分类号： F25B5/02 , B64D13/08 , B64D2013/0629 , B64D2013/0674 , F25B2600/2511
摘要： The present invention relates to an aircraft cooling system evaporator arrangement (10) with at least two mutually independent circuits (20a, 20b) for a coolant, at least two evaporation devices (12a, 12b) arranged to be hydraulically parallel for enabling an exchange of heat between the coolant and a refrigerant, at least two supply lines (18a, 18b) for supplying refrigerant to the evaporation devices (12a, 12b), and at least two discharge lines (22a, 22b) for discharging refrigerant from the evaporation devices (12a, 12b). One of the evaporation devices (12a, 12b), one of the supply lines (18a, 18b) and one of the discharge lines (22a, 22b) is assigned to each coolant circuit (20a, 20b). There is provision that the supply lines (18a, 18b) and discharge lines (22a, 22b) assigned to various coolant circuits (20a, 20b) are arranged to be hydraulically separate in each instance and that furthermore at least one refrigerant sensor (24a, 24b) for monitoring a refrigerant state is assigned to each of the discharge lines (22a, 22b). In addition, the evaporator arrangement (10) further includes an expansion valve (16) which for the purpose of controlling streams of refrigerant through the supply lines (18a, 18b) is designed to be driven in accordance with the refrigerant sensors (24a, 24b).
摘要翻译： 本发明涉及一种具有用于冷却剂的至少两个相互独立的电路（20a，20b）的飞行器冷却系统蒸发器装置（10），至少两个布置成液压平行的蒸发装置（12a，12b） 冷却剂和制冷剂之间的热量，用于向蒸发装置（12a，12b）供应制冷剂的至少两条供应管线（18a，18b）和用于从蒸发装置排出制冷剂的至少两条排出管线（22a，22b） 12a，12b）。 蒸发装置（12a，12b）中的一个，供应管线（18a，18b）中的一个和排放管线（22a，22b）中的一个被分配给每个冷却剂回路（20a，20b）。 设置分配给各种冷却剂回路（20a，20b）的供给管线（18a，18b）和排出管线（22a，22b）在每种情况下被液压地分开，并且还有至少一个制冷剂传感器（24a， 24b）分配给每个排出管线（22a，22b）。 此外，蒸发器装置（10）还包括膨胀阀（16），其用于控制通过供应管线（18a，18b）的制冷剂流被设计成根据制冷剂传感器（24a，24b）被驱动 ）。
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公开(公告)号：US08721406B2
公开(公告)日：2014-05-13
申请号：US13001353
申请日：2009-06-23
IPC分类号： B64D13/00
CPC分类号： B64D13/00 , B64D2241/00 , Y02T50/56
摘要： An air duct for supplying ambient air in an aircraft includes an air inlet, a flow duct portion and a feed device that is devised to feed ambient air through the air inlet and the flow duct portion. A flow control flap closes the air inlet in a first position, releases a first flow cross-section of the air inlet in a second position and releases a larger second flow cross-section of the air inlet in a third position. The flow control flap is designed to not increase drag significantly in the second position while still enabling flow through the flow duct portion, while increasing drag to increase air fow through the flow duct portion in the third position.
摘要翻译： 用于在飞行器中供应环境空气的空气管道包括空气入口，流动管道部分和进给装置，其被设计成通过空气入口和流动管道部分供给环境空气。 流动控制翼将空气入口封闭在第一位置，将空气入口的第一流动横截面释放在第二位置，并在第三位置释放空气入口的较大的第二流动横截面。 流量控制挡板被设计成在第二位置中不会显着地增加阻力，同时仍然允许流过流道部分，同时增加阻力以增加通过第三位置中的流动管道部分的气流。
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公开(公告)号：US20100326105A1
公开(公告)日：2010-12-30
申请号：US12790284
申请日：2010-05-28
CPC分类号： F25B41/00 , B64D13/08 , B64D2013/0674 , F25B2400/0401 , F25B2400/0411 , F25B2600/0251 , F25B2700/2106 , F25B2700/2116 , Y02T50/56
摘要： The invention relates to a refrigerating device (10), in particular for an aircraft, having a refrigerant circuit, in which a refrigerant container (12), an expansion valve (14), an evaporator (16), a compressor (20) and a condenser (22) are disposed. To save energy during operation and to increase the reliability and availability of the refrigerating device (10), in the refrigerant circuit there is a compressor bypass line (26), in which a bypass valve (18) is disposed, and a refrigerant pump (30) that is disposed downstream of the condenser (22) and upstream of the evaporator (16). It is possible to dispense with the refrigerant pump (30) if the condenser (22) is disposed at a higher level than the evaporator (16) in the refrigerant circuit.
摘要翻译： 本发明涉及具有制冷剂回路的制冷装置（10），特别是用于航空器的制冷装置（10），其中制冷剂容器（12），膨胀阀（14），蒸发器（16），压缩机（20）和 设置冷凝器（22）。 为了节省运转时的能量，提高制冷装置（10）的可靠性和可利用性，在制冷剂回路中设置有配置有旁通阀（18）的压缩机旁通管路（26）和制冷剂泵 30），其设置在冷凝器（22）的下游和蒸发器（16）的上游。 如果冷凝器（22）设置在比制冷剂回路中的蒸发器（16）更高的高度，则可以省略制冷剂泵（30）。
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公开(公告)号：US09617007B2
公开(公告)日：2017-04-11
申请号：US13434396
申请日：2012-03-29
申请人： Marc Hoelling , Werner Rothammer , Jan Dittmar , Carsten Colberg , Wilson Willy Casas Noriega , Ozan Uluc , Sebastian Roering , Holger Wolf
发明人： Marc Hoelling , Werner Rothammer , Jan Dittmar , Carsten Colberg , Wilson Willy Casas Noriega , Ozan Uluc , Sebastian Roering , Holger Wolf
摘要： A system for controlling a cooling system comprises an operating state detection unit adapted to detect operating signals characteristic of the operating state of the cooling system and/or the operating state of a plurality of cooling energy consumers to be supplied with cooling energy by the cooling system and a database in which priority data dependent on the operating state and characteristic of the priority to be given to the cooling energy consumers in terms of the cooling energy to be supplied in various operating states of the cooling system and/or of the cooling energy consumers, is stored for a plurality of cooling energy consumers to be supplied with cooling energy by the cooling system.
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公开(公告)号：US09315272B2
公开(公告)日：2016-04-19
申请号：US13432733
申请日：2012-03-28
申请人： Marc Hoelling , Werner Rothammer , Jan Dittmar , Carsten Colberg , Wilson Willy Casas Noriega , Ozan Uluc , Sebastian Roering , Holger Wolf
发明人： Marc Hoelling , Werner Rothammer , Jan Dittmar , Carsten Colberg , Wilson Willy Casas Noriega , Ozan Uluc , Sebastian Roering , Holger Wolf
摘要： A system for cooling and/or heating aircraft devices to be cooled and/or heated includes a first individual cooling and/or heating system associated with a first aircraft device to be cooled and/or heated, a second individual cooling and/or heating system associated with a second aircraft device to be cooled and/or heated, a cooling and/or heating energy supply apparatus adapted to supply cooling and/or heating energy generated by the first and/or the second individual cooling and/or heating system to the first and/or the second aircraft device to be cooled and/or heated, a control device adapted to receive and process signals characteristic of the cooling and/or heating requirements of the first and/or the second aircraft device to be cooled and/or heated and of the load condition of the first and/or the second individual cooling and/or heating system.
摘要翻译： 用于冷却和/或加热待冷却和/或加热的飞行器装置的系统包括与要冷却和/或加热的第一飞行器装置相关联的第一单独冷却和/或加热系统，第二单独冷却和/或加热系统 与要冷却和/或加热的第二飞行器装置相关联的冷却和/或加热能量供应装置，其适于将由第一和/或第二单独冷却和/或加热系统产生的冷却和/或加热能量提供给 第一和/或待冷却和/或加热的第二飞行器装置，适于接收和处理特征于待冷却的第一和/或第二飞行器装置的冷却和/或加热要求的信号的控制装置和/或 加热和第一和/或第二单独冷却和/或加热系统的负载状态。
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7.发明授权Aircraft cooling system evaporator arrangement for two mutually independent coolant circuits 有权飞机冷却系统蒸发器布置用于两个相互独立的冷却剂回路公开(公告)号：US08584484B2
公开(公告)日：2013-11-19
申请号：US12675278
申请日：2008-09-01
IPC分类号： F25B7/00
CPC分类号： F25B5/02 , B64D13/08 , B64D2013/0629 , B64D2013/0674 , F25B2600/2511
摘要： An aircraft cooling system evaporator arrangement has at least two mutually independent coolant circuits, at least two evaporation devices arranged to be hydraulically parallel for enabling an exchange of heat between the coolant and a refrigerant, at least two supply lines for supplying refrigerant to the evaporation devices, and at least two discharge lines for discharging refrigerant from the evaporation devices. A different one of the evaporation devices, a different one of the supply lines and a different one of the discharge lines are assigned to each of the coolant circuits, and the supply lines are hydraulically separate from each other as are the discharge lines. At least one refrigerant sensor monitors a refrigerant state of each of the discharge lines and an expansion valve is driven in accordance with the refrigerant sensors to control streams of refrigerant through the supply lines.
摘要翻译： 飞机冷却系统蒸发器装置具有至少两个相互独立的冷却剂回路，至少两个蒸发装置被布置成液压平行，以便能够在冷却剂和制冷剂之间交换热量，至少两条用于向制冷剂供应制冷剂的供应管线 和用于从蒸发装置排出制冷剂的至少两个排出管线。 不同的一个蒸发装置，不同的一个供应管线和不同的一个排放管线被分配给每个冷却剂回路，并且供应管线与排放管线一样液压地分开。 至少一个制冷剂传感器监测每个排出管线的制冷剂状态，并且根据制冷剂传感器驱动膨胀阀以控制通过供应管线的制冷剂流。
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8.发明申请Cooling Of An Electronic Device In An Aircraft By Case-By-Case Single-Phase Or Two-Phase Cooling 审中-公开飞机中电子设备的冷却通过单相或双相冷却公开(公告)号：US20120000630A1
公开(公告)日：2012-01-05
申请号：US12995220
申请日：2009-05-13
CPC分类号： B64D13/00 , B64D2013/0614 , B64D2013/0674 , F28D15/0266 , H05K7/20354
摘要： Cooling of an electronic device in an aircraft by case-by-case single-phase or two-phase coolingThere is proposed a method for cooling an electronic device in an aircraft (11), comprising the following steps:circulating a coolant in a cooling circuit,cooling the electronic device (2) by means of the coolant, andin an aircraft outer-shell heat exchanger, emitting the heat taken up by the coolant. The coolant evaporates, at least partially, during the cooling of the electronic device (2), and condenses in the aircraft outer-shell heat exchanger (7). The coolant circulates in the coolant circuit by natural convection.
摘要翻译： 通过逐个单相或两相冷却来冷却飞机中的电子设备提出了一种用于冷却飞行器（11）中的电子设备的方法，包括以下步骤：将冷却剂循环在冷却 电路，通过冷却剂冷却电子设备（2），并在飞机外壳热交换器中发射由冷却剂吸收的热量。 在冷却电子设备（2）期间，冷却剂至少部分地蒸发，并且在飞机外壳热交换器（7）中冷凝。 冷却剂通过自然对流在冷却剂回路中循环。
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公开(公告)号：US20110151764A1
公开(公告)日：2011-06-23
申请号：US13001353
申请日：2009-06-23
IPC分类号： B64D13/00
CPC分类号： B64D13/00 , B64D2241/00 , Y02T50/56
摘要： The invention relates to an air duct (10) for supplying ambient air in an aircraft, comprising an air inlet (12), a flow duct portion (16) extending downstream of the air inlet (12) and a feed device (22) that is devised to feed ambient air through the air inlet (12) and the flow duct portion (16). A flow control flap (24) closes the air inlet (12) in a first position, releases a first flow cross-section of the air inlet (12) in a second position and releases a second flow cross-section of the air inlet (12), which is larger than the first flow cross-section, in a third position. The flow control flap (24) is so designed and disposed that a first surface portion (28) of the flow control flap (24), in the second position of the flow control flap (24), is aligned in the region of the air inlet (12) substantially parallel to an aircraft outer skin portion (18) is surrounding the air inlet (12), and that the first surface portion (28) of the flow control flap (24), in the third position of the flow control flap (14), is aligned in the region of the air inlet (12) at an angle to the aircraft outer skin portion (18) surrounding the air inlet (12).
摘要翻译： 本发明涉及一种用于在飞行器中提供环境空气的空气管道（10），包括空气入口（12），在空气入口（12）的下游延伸的流动管道部分（16）和进料装置（22） 被设计成通过空气入口（12）和流动管道部分（16）供给环境空气。 流动控制翼片（24）在第一位置关闭空气入口（12），将空气入口（12）的第一流动横截面释放在第二位置，并释放空气入口的第二流动横截面 12），其大于第一流动横截面，在第三位置。 流动控制翼片（24）被设计和设置成使得在流动控制翼片（24）的第二位置处的流量控制翼片（24）的第一表面部分（28）在空气的区域中对准 基本上平行于飞行器外皮部分（18）的入口（12）围绕空气入口（12），并且流量控制翼片（24）的第一表面部分（28）处于流量控制 翼片（14）在空气入口（12）的区域中与围绕空气入口（12）的飞行器外皮部分（18）成一定角度排列。
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10.发明申请COOLING SYSTEM FOR COOLING HEAT LOADS ON BOARD AN AIRCRAFT AND METHOD FOR OPERATING SUCH A COOLING SYSTEM 有权用于冷却飞机上的热负荷的冷却系统和用于操作这种冷却系统的方法公开(公告)号：US20090321062A1
公开(公告)日：2009-12-31
申请号：US12438489
申请日：2007-08-17
IPC分类号： F28F27/00
CPC分类号： F25B25/005 , B64D13/06 , B64D2013/0629 , B64D2013/064 , B64D2013/0674 , Y02T50/44 , Y02T50/56
摘要： A cooling system for cooling heat loads on board an aircraft comprises a cold producing device, a first cold carrier fluid circuit, which is thermally coupled to the cold producing device and is connected to a first heat load in order to carry off heat from the first heat load, and a second cold carrier fluid circuit, which is connected to a second heat load in order to carry off heat from the second heat load. A coupling system of the cooling system is adapted to selectively thermally couple the first cold carrier fluid circuit to the second cold carrier fluid circuit or thermally uncouple it from the second cold carrier fluid circuit. In a method for operating such a cooling system for cooling heat loads on board an aircraft, the first cold carrier fluid circuit is selectively thermally coupled to the second cold carrier fluid circuit or thermally uncoupled from the second cold carrier fluid circuit by means of the coupling system.
摘要翻译： 用于冷却飞机上的热负荷的冷却系统包括冷产生装置，第一冷载体流体回路，其与冷产生装置热耦合并连接到第一热负荷，以便从第一 热负载和第二冷载体流体回路，其连接到第二热负荷以便从第二热负荷传递热量。 冷却系统的联接系统适于选择性地将第一冷载体流体回路耦合到第二冷载体流体回路，或者使其与第二冷载体流体回路热分离。 在用于操作用于冷却飞机上的热负荷的这种冷却系统的方法中，第一冷载体流体回路选择性地热耦合到第二冷载体流体回路，或者通过耦合与第二冷载体流体回路热分离 系统。
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